Gyroscopic compass.



M. E. CARRIE, DECD.

F. G. CARRIE, ADMiNlsTRATon.

GYROSCUPIC COMPASS.

APPLICATION HLED MAR24,1903.

l Patented Jan. 15, 1918.

5 SHEETS-SHEET l.

CIl

'JUL

, ggmf.- 7W/wg; am z l a oznm WI. E. CARRIE, DECD.

r. G. cARRIE. ADMINISTRATOR.

GYROSCOPIC COMPASS.

APPLICATION FILED MARK 24. 1903. 1925366@ meme@ Jan. I5, 1918.

5 SHEETS-SHEET 2- NI. E. CARRIE, DECD.

T. G. CARRIE. ADMINISTRATOR.

GYBOSCPIC COMPASS.

APPLICATION FILED MAII. 24. 1903.

19%539666. IPAIADIAUI Jan. I5, T918.

5 SHEETS-SHEET 3.

IVI. E. CARRIE, DECD.

F. G- CARRIE, ADMINISTRATOR.

Gvaoscomc coMPAss.

APPLICATION FILED MARi 24, 1903- lppf@ Patented Jan.15,1918.

5 SHEETS-SHEET 4- GII/vue :LIDL

IVI. E. CARRIE, DECD.

F. G. CARRIE, ADMINISTRATOR. GYHosc'oPlc COMPASS.

APPLICATION FILED MAR. 24, i903.

Patented Jan. I5, i918.

5 SHEETS-SHEET 5.

sas an oracion.

MERN EDWARD l CARRIE, OF PHILADELPHIA, PENNSYLVANIA; FRANKLIN G; CARRIE, ADMINISTRATOR OF SAID MERVYN E. CARRIE, DECEASEID, ASSIGNOR OF FIFTEEN ONE-HUNDREDTHS T0 GEORGE A. ROSSITER, 0F BROOKLYN, 'NEW YORK.

GYROSCOPIC COMPASS.

Specification of Letters Patent.

Patented Jian. i5, tm.

^Applleation tiled March 24, 1903. Serial No. 149,tl00.

To all whom t may concern: g

Be it known that I, MERVYN E; CARRIE, a citizen of the United States, and resident of Philadelphia, county of Philadelphia, and State of Pennsylvania, have made a new and useful inventlon in Gyroscopic Compasses, of which the following is a specification.

'llhis invention comprises a. mechanism for automatically and continuously indicating latitude and longitude, as well as the position of either of the poles of the earth at any point on the surface thereof, and has for its object, lirst, -to give constant and correct indications regardless of natural conditions; second, to render less necessary the usual nautical instruments; third, to provide a device for compensating for friction and lost motion, so that the movements recorded and indicated will be correct.

For a full and clear understanding of my invention, reference is had to the accompanying drawings, forming a part of this specification, in which- Figure 1 is a part longitudinal sectional, and part side elevational view illustrating the controlling appliances of the apparatus;

Fig. 2 is a part transverse sectional, part plan view ofthe same as seen looking at Fig. l in the direction ot' the vertical arrows on the right and left, with certain parts omitted;

Fig. 3 is a detail view of a dial and pointer for adjusting the gyroscope frame Fig. 4 is a part diagrammatic, and part end view of that part of the controlling apparatus seen looking at Fig. 1 from right to left in the direction of the horizontal arrows;

Fig. 5 is a part perspective, part sectional view of the table and supporting attachments for the entire controlling apparatus, the upper ends of the sustaining or supporting standards to which the same is pivotally supported being shown in side elevation;

Fig. 6 is a detail perspective view, partly in section, oi' a part of the supporting table for the gyroscopes and the frames in which they are pivoted;

Fig. 7 is a part perspective, part diagram- Amatic view ofv a train of mechanism for operating the indicating and recording devicesl Figi. Sis a detail diagrammatic view etk a ratchet and pawl mechanism Awhich may be utilized in the apparatus for effecting step by step movements;

Fig. 9 is a perspective View of tbe chart table upon which the latitude and longitude arev indicated and recorded,'the recordin stylus also being shown above the center o the table;

Fig. 10 is a vertical sectional view illustrating the modified form of electro-motive controlling apparatus for adjusting the gyroscope frames and eifecting certain movements of other parts of the apparatus;'

Fig. 11 is a part diagrammatic, part end elevational view of a mechanism such as that disclosed in Fig. 10, and upon the supposition that a single lnotor is used and the armature thereof made reversible in its rota-y tion;

Fig. l2 is a diagrammatic view of a modied form of circuit breaker for the compensating mechanism shown in Fig. 4:;

Fig. 13 is a part perspective, part diagrammatic View illustrating diagrammatically so much of the complete system as will enable one to understand its operation as a whole; and

Fig. 14 is a view illustrating a dial mechanism comprising a pair of magnets, a lever, a ratchet and a pair Dt pawls.

Referring now to the drawings, in detail,

A, Figs. 1 and 2, represents a balanced frame or support in which two gyroscopes are mounted and adapted to rotate. The supporting frame is substantially rectangular 1n form, although its particular form is non-essential, and it is provided at each end with short shafts bearings or arbors a, a5, on which it is adapted to turn or oscillate freely. These arbors a, a5 are supported in proper journals or supports carried by the two vertical posts or standards al a, which in turn are supported on a table T carried by a float, free to turn in azimuth, and held in a horizontal position by a pendulous system comprising the gyroscopic disks J1 and J'2 all as will appear below.

lin the frame A are mounted two gyroscope disks, B and C, one of them preferably larger than the other, B representing the larger or latitude wheel or gyroscope disk, and C the smaller or longitude wheel or disk. ll have represented the disk B as mounted in therear or lett end of the said lltlti supporting frame A, and C as mounted in the front or right hand end of sa1d frame 1 A, but these positions may be reversed and the o eration would be precisely the same. The isk B is mounted on the shaft or arbor b, b, so as to be rotated 1n a plane parallel` with the length of the frame A, and the disk C at a right angle thereto, on a shaft or arbor c c. These said shafts or arbors have their bearings in the supporting frames A and A as shown.

Suitable motors l, Z, are used for rotating the yroscope disks B and C and they are revolved at a very high speed. Surroundlng the supporting frame A is a second or lati.-

' tude frame D which is substantially annular in form, and centrally thereof at each end said second frame is provided with stub shafts al and d, which turn easily in journals in the posts or supports a1, a6. These shafts d, d, are bored .through axially, as shown, so as to constitute journal bearings for the said additional short shafts a and a, above mentioned. The shaft (l shown on the right in Fig. l, constitutes a rigid support for a wheel E which coperates with certain connections to be hereinafter described, their function being to compensate for friction and lost motion. To the extreme right hand end of this said stub shaft d, Fig. l, is also secured. a yoke or fork F which may, if preferred, be insulated from such shaft (see also Fig. 4).. An arm or tongue f is secured tol the right hand or front shaft a of the supporting frame A, so as to turn therewith and is insulated at its point of connection therewith, as will be clear from Figs. l and 4. At its outer endv the tongue f is provided with a cross arm f1, extending substantially at right angles to lts length. At the inside ends of the yoke or fork F are carbon buttons f2, f2 with which the cross arm f1 is in loose electrical contact, so that the resistance of the said contacts is increased or diminished by pressure as the arm f turns with the shaft a. From what has now been disclosed it will be clear that the pendulous weights comprising the gyroscopic disks J1 and J 2, will keep the table T always horizontal and the standards or supports a1 a vertical. It will also be clear that if the second or latitude frame D be arranged in a vertical plane, t will likewise remain vertical with the standards a1, as until moved out of said plane, and that said standards and frame may be readily turned in azimuth so that the plane of rotation of the latitude disk B may be made parallel to the plane of the -tailestial equator. Accordingly, it is also evident that if the parts are ositioned asjust stated and the instrument 1s carried due north, owing to the` tendency of the rotating gvroscopic disk B to maintain a plane parallel to that of the equator, the plane of the lbearings or arbors a, a

and pivots b, b, as well as of the frame A will not turn the curvature of the earth, but will remain in a plane perpendicular to that of the equator. The plane of these parts will however turn with the curvature of the earth when the instrument is moved due east or west, as will appear below. On the other hand the standards a1 a" will turn with the curvature of the earth as the latitude changes so as to always lie in the vertical plane of theplace. It therefore follows that as the instrument proceeds due orth or due south, a slight turning movement of the short shafts d and d about or over the bearings or arbors a and a", will take place, and any friction that may be engendered in this turning movement will tend to rotate the said bearings or arbors a and a5 and therefore the disk B out of its plane parallel to the equator. Of course, it will be understood that the degree of movement of the fork F with the shaft d is small, and therefore the movement of the arm with the cross piece or arm tive to fork F, but 1t will he clear that the pressure of one end or the other of the arm f1 against the carbons f2 f2 is due to the turnlng of the frame D while changing its latitude caused by the curvature of the earth; and the means by which the friction thus engendered is compensated for through the medium of the wheel E, between the stub 1s very minute, rela las shaft d, and the shaft or support a, is as follows:

A suitable motor G is located at a proper point and carries a shaft. which is practically iexible by virtue of lts being provided with a universal joint Two magnets G G are located between the motor and the wheel E. An armature g is elastically supported ona suitable frame over the magnet G and the shaft g is passed through or attached to the armature g and extended toward the wheel E between the bifurcated or slotted support g2 having astop pin or lug g3 to limit its upward movement. The rear end or part of the shaft g nearest the wheel E has rigidly mounted on and adapted to rotate with it, a friction wheel g4 which, under certain conditions, engages with a friction wheel g5 mounted on a shaft g6 which is supported in suitable standards g7 g8. On the end of the shaft g" is another friction wheel gf which is always engaged with the wheel E. The frame or bracket carrying theA other armature 9"v is preferably composed of two angular .members v nauseas ln Fig. 4 of the drawings l have shown the connections to the wheel E and itsfork as derived from the two electromagnets G G and a suitable battery BA, interposed at a proper point in the line, but I do not limit myself to any source of electrical .or electromagnetic supply. A main and a branch line from a dynamo, for eX- ample, would produce the results desired and perhaps in most instances would be the means employed. To the two arms or prongs of the fork F adjacent to the carbon buttons are two wires y, z, the Awirey extending to one coil of 'a differential galvanometer w and the wire a to the other coil thereof. The dial of the galvanometen as usual, is provided with a needle or pointer w and also with two metallic stops w" fw for the needle as it is moved in one direction or the other by the current. The current on the wire {1/ passes from one prong of the fork F through the coil of the galvanometer to and throughthe battery BA back through the arm f tol one arm of the fork F, thus completing this circuit. The

current on the-wire passes from the other prong of the fork F through the other coil of the galvanometer w yto and through the same battery, through the arm or tongue f to the fork F. As the pressure of the cross arm on the carbon buttons is variable, it -will be apparent that the resistance and strength of the currents are also variable', and that. the needle of lthe galvanometer will be deflected to one or the other of the stops fw fw as will be described later on. The galvanometer is not absolutely essential with the connections just described, as any properly operated circuit breaker may be substituted therefor, and in Fig. l2 I `have shown a substitute apparatus for the same purpose which will be presentlydescribed. Referring'again to Fig.' 4, a second battery B1 A1 isl suitably located and properly connected with the ele'ctromagnets G G for energizing them. The wire y eX- tends from the battery to the needle pivot and the current passes through the needle itself, to the stop w. i From stop w the eurrent passes to the electromagnet G and thence back to the battery, thus completing the circuit. A second current over Wire y passes from the battery to the needle pivot through the needle Awhen deflected to the left. or to the stop w, and from this point to the electromagnet Gf and thence back to the battery when the pressure against the carbon is greater on theprong f4 of the fork F than it is on the carbon carried by the other prong f3.

In other words an increased pressure 'on the carbon f2 of the south arm f3 of the fork F causes an increasing flow of current which enters the arm or tongue f from the battery BA, byA the conductor and passes -which the arbors alo out mainly through this arm f to the galvanometer and detlects the needle to the stop 'w' which permits the current flow that enei'gizes the magnet G. The armature g' is thereupon drawn down and depresses the friction wheel (14 driven by the motor Gr and brings it into` operative driving connection with the periphery of the wheel g5 thus reversing the movementof the wheel E, and compensating for any-frictional rotary force that may have existed between the bearing t and shaft d. long as the pressure is greater at the south arm f3 ofthe fork F, or until the pressure is equalized, whenv the deflection of the needle ceases. If the pressure at the north arm f4 of the fork F is the greater, then the current entering the arm or tongue f from the battery BA passes out through said arm or tongue f4 to the galvanometer, deflecting the needle to stop fw and closing the ycircuit, thus carry currentwhich energizes the magnet G. The armature of this magnet is drawn into contact and the friction wheel (114 is brought into operative mechanical or t'rietional connection with the Wheels g4 g5.

rlhis mechanism accordingly operates to turn the wheel E in a reverse direction from that before described.

lt will now be clear when the second frame D owing to the curvature of the earth is slightly moved from the plane of rotation of the disk B toward'a vertical plane making an angle with said plane of rotation, and thereby generates more or less friction between the shaft d and bearing a that an increased pressure will be'exerted on one or the other of the carbons f2 f2 and the wheel E will be turned in a direction opposite to that caused by the curvature of the earth, so that said friction will be compensated for. In other words, it will now be plain that I have provided a sort of frietionless support in the bearing rt and shaft d.

The frame D serves the purpose of transmitting the relative movements duo, to the earths curvature to the opposite end of the gyroscope frame. But it will be understood that for this purpose half of this frame would be sutlicient; that is to say, a frame of arch form, but as it is essential that it be counterbalanced for the delicate adjustment required I construct it preferably in the form of an annulus, as shown. The two end shafts or bearings d and d5 being rigidly connected move synchronously.

The longitude gyroscope and its coacting parts will now be described. The longitude disk C is mounted on the tilting frame A having arbors or supports al a, Fig. 2, and associated therewith is a third frame D1 having hollow arborsor shafts all d through a respectively pass. la10 is an arm f1 diain'Fig. 13 and `in all Rigid with the arbor grammatically shown This operation continues as respects the same as the arm f associated with the bearing or arbor a, and rigid with the arbor d1 is a wheel E10. Fig. 3 in all respects the same as the wheel E associated with the stub shaft arbor while a forked arm indicated at F10 is carried by albor d10 in all respects the same as arm F. In fact associated with the members just described are duplicates. not fully shown, of the members or devices above disclosed for compensating for friction between the bearing a and shaft d.' so that friction between the arbors or supports am and d10 is compensated for in connection with the disk C by means (not fully shown) which are or may be a duplicate of those employed in connection with the disk I5. Or` in lieu thereof I may use an alternative form of mechanism which I design to use for both the latitude and longitude disks, if desired, as will be hereinafter described- It is evident that when the instrument is carried due north or south in the plane of a meridian the plane of the frame A. and axis b b remains perpendicular to the piane of equator; while owing to the pendulous suspension comprising the disks J1 and J2 the plane of the posts (1.1 and a becomes inclined to said plane, to an extent depending upon the change in latitude. It is also evident that the latitude frame D would also become inclined to the plane of the equator if its slight rotations due to the curvature were not constantly corrected or destroyed by the friction compensating mechanism disclosed.

It will likewise now be clear that, if the vessel moves east or west, the parts are in the positions above supposed, and although the said north and south plane of the axis Z) b remains fixed or perpendicular to the plane of the equator, as just stated, yet, the plane of frame A and of the arbors or supports a a5 will be tipped in an east and west direction at an angle to the original plane of the meridian owing to the curvature of the earth, and that the extent of this tipping will depend upon the change in longitude. It should here be remarked that the only friction generated by the frame D which is not counteracted is that occurring between the journals carried by the posts a1 and a and the stub shafts d and d5 respectively; and that this latter friction does not tend to move the disk B out of its original plane.

Again, it will be clear that were it not for the friction compensating devices associated with stub shafts d10 and d, the longitude or third frame D1 wouldlikewise change its initial inclination to the plane of the original meridian as the vessel changes its longitude. The frame A1 however, being journaled as illustrated in the frame D1 will not partake of this motion because the disk C will hold it in its original plane, perpendicular to that of the original meridian, and therefore the above relative movement between the arbors am and d10 will take place.

Again in the case of the latitude bearing or arbor a5 it remains stationary while changes in latitude cause the stub shaft d5 and its supports or journal a, to turn for changes in latitude, so that contacts such as it and 71,1 on a wheel H-rigid with said supports will likewise turn or change their vertical planes as the latitude changes, and will contact with an arm I carried by the bearing or arbor 0.5. longitude will cause similar contacts 71,10 and 7L (see Figs. 2 and 13) on a wheel H10 to change their meridional planes and to have contact with an arm Il carried by shaft or arbor all. By the means just disclosed and their cooperating mechanism the latitude and longitude is or may be indicated and recorded, at a plurality of places aboard ship as will now be made plain.

The general idea of the utilization of like or duplicate parts of the controlling appliances which are designed to perform the several different functions, in connection with the complete apparatus, may be had from the diagrammatic view illustrated in Fig. 13 to. which specic reference will be had later.

Referring now to the specific details of the controlling appliances for indicating and recording latitude H is the wheel for operating or controlling the recording and indicating mechanism, the letter H10 representing like parts as applicable in connection with the longitude gyroscope disks C. This wheel H is mounted on a standard H which supports a short shaft H2 on which the wheel turns or rotates (see Figs. 1 and 7) and therefore the plane of the axis of this wheel will remain in a vertical plane. On the inner face of the periphery of the wheel H, or at any suitable point thereon, are two stops h it insulated from the wheel itself.

An arm I is rigidly secured to the end of the bearing or arbor a5 at the left of the gyroscope frame A and remains stationary with said frame. This arm I is insulated from the shaft a and wheel H and is connected by a flexible conductor at its upper end to a battery B2 A2, Fig. 13. When the movement of the wheel H owing to the curvature of the earth, during changes in latitude brings the arm I into contact with the stop 7L it indicates a higher latitude, while its movement causing a contact with stop it indicates a lower latitude. These movements are indicated on proper dials, through the medium of mechanism which I will now proceed to describe. The two electromagnets N N1 are mounted on the gyroscope table T in suitable proximity to the wheel H and about midway between the two mag- In the same way, changes Vof n secured thereto at each side of the A shaft H7 has bearings in the-support H and on the end thereof is a ratchet Wheel h4 with which either of the pawls h2 or ha is adapted to engage as one or the other of the armatures is brought into contact with one or the other of the electromagnets N, N1. At the other end of the shaft H7 which is supported by the standard H1 is a plain wheel or roll H8 which is in frictional engagement withthe wheel H, as will be hereinafter explained. Similar mechanisms of substantially the'same character as that just described are located at proper places in the pilot house, one tov be used in connection with indicating dials, and the others for operating the chart table and other appliances to be hereinafter described.

K represents one of the mechanisms and M a dial with its needle or pointer lP which is operated thereby.. L represents another of these mechanisms which is providedY with l a rack and gear for operating the chart table (see Figs. 7, 9 and 13). This mechanism L, so far as the electromagnets, armatures, pawls and ratchets are concerned, is pre cisely'the same as already described wherever used inr the complte system. Instead, however, of having a smooth friction wheel at the end of the shaft H2, opposite the ratchet wheel, it is in this instance provided with a gear wheel whichrmeshes with a toothed rack Q1 for moving the chart table back and forth.

The means for operating these three mechanisms is as follows z-Starting from a point on the arni T (see Ijig. 7) the current from the battery B2 A2 passes through the arm to the pin h with which it is shown in very light Contact on the drawings; thence inmultple by means of branch circuits to the left hand electromagnets H3 N2 of both the dial and chart operating mechanisms, back to the battery B2 A2 and through the same to the arm I, thus operating the needle P of the dial and simultaneously moving the table by the movement of the racky bar, and indicatingand registering the change of movement of the vesselto a higher latitude, primarily through the movement of the contacts it and L on the Wheel H the left hand ends of the armature in the Vmechanisms, L and K, are both in contact from the battery B3 A3 by way of the pole of the magnet H3, armature H, armature of the dial mechanism M, pole of magnet'N2,

magnet N1 back to the battery. This action, therefore, causes the armature rH to be .change to a lower latitude,

produced by the curvatureof theearth. It will' 'be seen that in the operation just described drawn into the position shown in dotted lines, thereby imparting motion to the shaft H" and roller H", and, consequently, to the wheel H, .rotating the, arm T .to the lett and breaking or varying the circuit between arm T and contact h so as to operate the indicatteeth the pawl k2 not only simultaneously ascends the same distance and therefore does not prevent the wheel it* from rotating but it moves out of the path of its associated ascending tooth, so that the latter slips past said pawl h2. Ot course, any other suitable device may be substituted for these part-s. For indicating and recording the when the arm ll readily is in contact with the in k on wheel H, i

the same character of circuits are used, eX- cepting that the currents are passed throu h the right hand magnets H4 Na instead ot' t e lefthand magnets H3N2, thus reversing the direction of the needle on the dial and the movement ofthe chart table, and further description thereof will therefore be unnecessary.

The mechanism now disclosed will malte it plain that changes of latitude are readily indicated at a plurality of places on ship board, by the tol and fro movements of .the contacts k and k1 corresponding to changes in latitude, relative to the arm lt carried by the latitude arbor a5, and by the rotary movements imparted yto shafts such' asl-ll" and pointers such as P as well as by reciprocating movements imparted to racks such as @5 all as a result of circuits closed by said arm I and contacts h and k1. It will also be evident that duplicate mechanisms or devices are provided in connection with the longitude arbor al?, arm T10, wheel ll- 1 Aand contacts. iemand la, the latter being shown in Fig. 13.

These latitude and longitude indicating devices when lin the form of racks Q1 are readily assembled at right angles to each otheras indicated in Figs. 9 and 13, to oper.- ate a chart table. This table is generally mounted in theV ilot house and is preferably'- rectangular in orm, although the particular configuration is not essential. 'It comprises three parts or members 0', O2 slidably mounted one above the other. The lower member O2 is relatively xed and near its ends are vertical supports o2 02 which receive the member O at some distance above the base or member U2. The under side of the member O has grooved cleats and the supports o2 are tongued and lit in the grooves in said cleats, so that the part Of may slide TGI llllG lill@ freely in two directions; that is to say, back and forth on these supports. The top of the part also has vertical tongued supports osimilar to thel supports 02,- b'ut they are arranged at right anglesthereto. The top member or part() has corresponding grooves for the tongues o and the arrangement is such that the top member O also has a back and forth movement, but at right angles to the member O. Between the tables O, O and also between tables O and O2 are mounted the various mechanisms already described and represented in Fig. 7 for operating the table and for indicating the latitude and longitude respectively, and these areas a matter of course arranged at right angles to each other. Siphon recorder, or analogous device St is mounted as shown, above the table and records or traces all the changes of the movement of the vessel thereon. In practice a sheet of paper, linen, a coat of carbon or graphite, or any chart is used on the table for such tracings. In view of the fact that the longitude gyroscope rotates in a plane of a meridian and would have its plane of rotation turned through 3600 in one day or 15 per hour, owing to the earths rotation, I have provided a. 24 hour clock mechanism Q (see Fig. 13) sustained by one of two standards J which support at their upper ends the frame work R that sustains the stylus St. The hour shaft of this clock is connecteddirectly to a screw 80 which passes through a screw-nut sa connected directly to the stylus, the arrangement being such that the clock mechanism keeping accurate time necessarily gives a correct indication of the time when the sun crosses the meridian above and below. The hour shaft of the clock mechanism and screw attached thereto rotates in the proper direction to cause the stylus St to move in a'reverse direction to the movement successively imparted by the longitude mechanism L to the chart table O. In other words, if the vessel is in port it is obvious that inasmuch as the longitude mechanism is always successively moving the chart table O from west to east, the clock mechanism will be simultaneously moving the stylus St in such a direction that so long as the vessel remains in port or is absolutely stationary no registration of longitude will be4 effected on the chart table.

Fig. 5 of the drawings shows the table for supporting the gyroseopes and their frames as well as the friction compensating mechanism and the wheel and arm through the medium of which the indicating and registering mechanism is operated or controlled.

The view is a central vertical section. The

A suitable pointer, stylus,v

figuration of the underside of the base T2,

which base is supported by a frame T2.

As will best be seen from Fig. 6, the table T is provided with an insulated contact member f adapted to make contact with a pair of insulated contact F carried by the supporting base T2. The currents controlled by the contacts f F serve to operate the motor driving the shaft 5, as will appear below.

This frame T3 is pivoted at two points to a ring or annulus Ta, which ring is resiliently and delicately mounted on the two vertical supports Tb, Tb by means of knife edge bearings tf t', Fig. 5 and the spiral springs 152. The table T and base T2 are pivoted to each other by means of the short pivot t* which is securedto the base T2 and moves freely in a bearing in the center of the table T. Suitable ball bearings are used between the table and base and also between the base and the trough shaped frame T3 for the purpose of overcoming friction and making the adjustment very sensitive, as clearly shown. The base T2 has on its underside al centrally arranged shaft t5 on' which are wound two rotary armatures t t7 within magnetic fields ts t9 of two rotary motors for thel purpose of turning the sha-ft' t5 in opposite directions from time to time. These field coils are supported by a suitable tubular extension T4 attached to or forming a part of the trough carrying frame T3. On

the bottom of the shaft t5 is attached an arm tu substantially the saine as the arm I above described. in connection with the wheel E, and the latter has its counterpart in a wheel T5 carrying the contacts T20 and T3". The wheel 'I5 is mounted to be turned on a suitable pivot or stub shaft in the bottom of the tubular extension T4. It will be seen that this arm and wheel are similar to the wheel H contacts it and h1 and arm I (Figs. l, 7 and 13) excepting that they are arranged horizontally instead of vertically. The arm and wheel just described and the means for operating the same, being substantially like the corresponding mechanism indicated by the letters K and L, Fig. 7, show by means of a proper dial and pointer, such as M and P located inthe pilot house changes in position, in the same manner that the wheel E, arm I and connected mechanism indicate latitude and longitude, thus simulating a compass in its operation. For example, the turnlng of the table T upon whichI the gyroseopes and appendages rest, in either direc-I tion in a horizontal plane, may be detected and electrically and mechanically transmitted to the dial M shown on the extreme left aaaaeee hand side of Fig. 1?: and situated in the'pilot house or elsewhere, precisely as the deflections of the latitude gyrosco es are detectedy the arms I,A

transmitted and indicated I stops z. k1, wheels H, conducting wires, ratchet and dial mechanism M, F1 7. It will be remembered in this connection that, the' aXis of the latitude gyroscope B when properly set and in operation is always parallel to the axis of the earth, and that the gyroscope disk B itself, when in operation, always rotates in aplane paralle with a plane passing throug the'equator, so that if thevessel is traveling east or west on the equator this gyroscope B will be rotatlng exactly in said plane.

From the bottom or underside of the tubular extension T* depends another shaft t. and on this shaft are two heavy gyroscopic disks J1 J 2 arranged in a horizontal position and adapted to be turned in opposite directions by suitable electric motors Ta T7 operatively connected with the independent batteries b a and b1 a1' (see Figs. l and 13 These disks are for the purpose of yiel vingly maintaining the table always 1n a horizontal plane. It is pertinent to remark that a gyroscope retains its plane of rotation, only when freely suspended and free from outwardly impressed mechanism disturbances which, of course, implies :that the lines passing through its points of suspension shall also pass through its center of gravity. These conditions are true of the latitude and longitude gyroscopic disks B and C but are not true of the gyroscopes suspended beneath the table, and well below the 4center of gravity of the table and the apparatus upon it. Inasmuch as these lower gyroscopes J1 J2 have weight they act as any other dead weight would act in preserving the horizontality of the table. dition to this they resist swaying disturbancesto the table caused by sudden shocks from the rolling or pitching of the vessel, the vibrations of the engine, ctc., as dead weight would not do; for a gyroscope will violently resist any sudden effort to change its place of rotation while it yields perfectly to any gradually impressed force. Tt is this last mentioned property of yielding to gradually impressed force (in this case gravity) that allows the disks J1, and J 2 to hang vertically and in no way interfere with' the change of plane' of the table T owing to` the curvature of the earth, and to changes in latitude and longitude.

In Fig. 8 of the drawings I have shown the ratchet and pawl mechanism by which the step by step control is effected. The ratchet and pawl mechanism illustrated in Fig. 7 is shown on an exaggerated scale and diagrammatically so as to give a. better illustration of the circuit relations of the parts. As illustrated in said Fig. 8, when either In adof the pawls is depressed, under the intluenceof its corresponding magnet, it will rotate the ratchet wheel h4 throu h a distance of two teeth so that when t e armature H is released by that magnet the two pawls by their own weight will assume the position shown. Therefore, no matter which pawl be operated upon the shaft H7 will be rotated in the proper direction.

Figs. 10, l1 and 12 show modified forms of mechanism which may be used in lieu of the mechanism described in detail for overcoming the friction and lost motion.

In Figs. 10 and 11 T have illustrated a modified form of mechanism for taking the place of the mechanism for compensating or friction disclosed in Figs'. 1, 3 and 13, and whereby the movement of the wheel E in opposite directions is effected. Tn these Figs. 10- and 11 of the drawings two electric motors are shown embracing stationary field magnets lPlA P1 secured to the frame and rotary armatures U, U, the latter sustained by they shaft or bearing d of the frame D. To the outer end of this shaft l is connected and insulated therefrom a fork F and to the shaft or arbor a and arm f, also insulated from the shaft.

The circuit, however, is did'erently arranged but has a similar function and mode of operation. The circuit starts from a battery B4 A* suitably located and branches to each of thed'eld magnets P1, P1 of the motors U, U and passes through the same, extending' to the ends of the fork of arm F adjacent to the carbon buttons. From oneI or the other of these buttons, or both, it passes to the cross arm carried by arm j' and thence back to the battery. The motors being excited tend t0 turn the sleeve in op- 10 posite directions, with forces corresponding to the pressures on the carbon buttons. This mechanism may be used in the same manner as that described in that part of the specification which refers to the equivalent lll mechanism shown in Fig. 1. This mechanism may also be used for the longitude disk, it being obvious to those skilled in the art that the circuit arrangement illustrated in the apparatus represented by the letters Kand L, Fig. 2 may be so arranged as to adapt the same for the use of such motors in place of the step by step mechanism illustrated. Two motors lare shown in Fig. 10 ofthe drawings, but ifa motor should be used at each end of the frame D it would be single instead of double.

Tn F ig.l l1 I have shown the same structure as that shown in Fig. 10, but with a single motor used in connection with a galvanometer or suitable circuit breaker, so that by the use of a single motor the direction of the current flow, and hence the movement of the arm 7, may be reversed. The circuits are arranged in a well known manner on the drawing to produce this result, and need no explanation.

Fig. 12 represents a mechanism which may be used in place of the galvanometer shown and described. It comprises means for making and breaking a circuit and it is represented in this view as connected with fork F and arm f. It consists of two electromagnets Sv, S2 arranged in such relation that their poles are opposite each other with an armature S1 between them. This armature is carried or supported by a spring arm s and may thus be brought into contact with one or the other of the magnets as they are energized. The circuit is formed in the same manner as in the case where the galvanonieter is used and the description thereof need not be repeated.

The operation of the mechanism will be' clear from the foregoing, but may bel summarized as follows: Having been suitably arranged onboard ship, the gyroscope table T is adjusted so that the axis b b of disk B will point due north and south (see Fig. 2). The plane of the gyroscope B is by means of the dial and needle, Fig. 3, inclined in to a plane parallel with the plane of the equator and at an angle to the vertical plane equal to the latitude of the place of starting. The latitude and longitude dials are adjusted to the latitude andlongitude of the starting point and the chart table is so adjusted as to bring the pointer, stylus, or Siphon recorder St to that point upon the chart or map-correctly placed-upon the table-which represents the' latitude and longitude of the starting point. All the electric motors which control the movements of the apparatus are then set in motion, those motors which continuously drive the gyroscopes being given a very high velocity.

The latitude gyroscopic disk B by its varying inclination to the vertical, due to the earths curvature, as the vessel proceeds on her course, will transmit to the latitude dial and chart table the changes in latitude, through the indicating and recording mechanism. In like manner the total rotation of the longitude gyroscopic disk C, comprising that portion due to the earths rotation and that due to motionof translation along with the ship east or westvof the meridian of the starting point, is transmitted/to the longitude dial and chart table, while the clock mechanism Q, Fig. 13 corrects that portion of the readings due to the earths rotation,

and thus is indicated and recorded the changes in longitude. The composition of the'two movements, due to changes in latitude and longitude, respectively, gives in the curves traced by the pencil, stylus, or Siphon recorder the precise course of the ship. The original north and south direction given to the latitude gyroscope B is preserved, owing to the tendency of the rotating disks to preserve their planes of rotation assisted by the mechanism for compensating for friction and lost motion in a horizontal plane. It will, of course, be understood that the gyroscope frame with its gyroscopes and attachments is mounted on the freely movable table T supported by the mercury, and which table is located at any suitable place on the vessel, preferably at some point amidships. It will also be apparent that the chart table and the latitude and longitude dials are preferably located in the pilot house.

In view of the description heretofore given, a critical examination of Fig. 13 will disclose the fact that so long as all of the gyroscopes are continuously rotating and the 24 hour clocks correctly adjusted and set for the longitude from which the vessel is sailing, the mechanism will continue to indicate on the latitude and longitude dials the latitude and longitude in degrees and record on the chart table the actual latitude and longitude. At the same time, as the vessel proceeds, any change of direction will cause the polar indicator M, shown on the extreme left lhand side of Fig. 13 of the drawings, to give a correct indication of the number of degrees of 'such change, either east or west of the north point, or east or west of the south point, it being apparent that the exact polar indication on a controlling apparatus amid-ship will be given by the arrow NS (see Fig.. 2) on the base of the instrument, as obviously, if the controlling gyroscopes B and C be kept moving this indication will never change. lt will, also be apparent that the gyroscopes J1 and J2.

other apparatus to efectually, balance the controlling apparatus above, will maintain the delicately pivoted supported means of control always in the position of starting.

From the foregoing it will be apparent that the arrow N S, the axis bb or any other part of the mechanism may be properly oriented whenthe motor is started and thus constitute a means for indicating the -true north or any other point of the compass. In the same way, the pivot T4 or any other part of the frame may be pointed to the head of the ship and thus constitute a lubbers point by which the course is determined. It will also be clear that the mechanism disclosed provides a gyroscopic disk such as B associated with bearings, in this instance, exemplified by the arbors a and a5, which bearings are in turn associated with the journals or standards al and as; that said standards are supported on the horizontal table T and that said table is supported on the ball bearings and mercury float illustrated, which in turn are supported on the Magee@ gimbal mountings and standards Ts resting on the deck of the ship. Tn other words, the parts a, a, al, a", T, T, constitute in this instance a support for the disk B which comprises friction surfaces between said parts a.d and a1 for example, and also friction surfaces between the horizontal table T and its associated ball bearings.

Tt will also be apparent that as friction is generated at any bearing such as a for eX- ample, it will be automatically compensated for as the disks B andl`- C move over the earths surface by the mechanism comprising the arm F and its associated parts.

It will further be clear that the above mechanism rovides contacts f, F associated with the ta le T controlling circuits to an automatic friction compensating mechanism similar to that just mentioned, and which last named mechanism compensates for any errors of the compass due to friction enendered when the ship turns in azimuth. aid mechanism further provides a vertical shaft 155y having an arm 151 adapted to make circuit with the contacts T20 and Tf, which Ycircuit controls indicating mechanism similar to that constituted by the parts H, H

' H7, H", h3, h4, etc. It willlikewise be clear thaty the gyroscopic pendulum will act differently from a pendulum consisting of dead weight only, in that it will not readily respond to the rolling and itching movements `of the shipias would a c ead weight pendu# lum, but will resist sudden motions of this kind, and therefore, while compelling the table T to assume a horizontal position as vthe ship moves over the earths surface, yet

it will stabilize or tend to maintain substantially horizontal the table T, or'other horizontally disposed member, even though the 'ship pitches violently.

Tn other words, the parts A, a1, a, T, T8, T4, T, etc., in the instance illustrated constitute a. pendulum supportin means for the oscopic disk B t at is adapted by its dea weight to assume a normal fixed position relative to the horizontal plane as the ship moves over the earths surface, while the gyroscopic disks such as J1, J2 associated with said supporting means constitutes in this instance, an example of a stabilizing gyroscopic device, of general application, adapted to prevent errors of gyroscopic compasses due to the rolling and pitching movements of the ship. Stated in still other language, in the'instance disclosed, as the shi moves over the earths surface the dead weight of the parts mentioned will cause the table T or other horizontally disposed memv ber, to automatically assume a horizontal plane and the standards a1 a to automati- I cally assume a vertical plane as each new position is reached, while the gyroscopic disks such as J1 J2 will stabilize said parts in their respective planes as the ship rolls and pitches.

The invention may be used with facility in making surveys of coast lines, as well as for other purpose where the exact latitude or longitude is required, and while the mechanism above described is the best form known to me, minor changes may be made within the scope of my invention without departing from the spirit thereof or sacriicing any of the advantages thereof.

Therefore I do not limit my invention to the details of construction shown in the drawings and hereinbefore described for determining the position of a. moving vessel or body upon the earths surface, through the agency of gyroscopes kept in continuous rotation, and for thereby edecting a cordinate indication orcordinate registration of such point o'r location, as my claims hereinafter are to be construed as of the most generic nature with relation to the utilization of gyroscopes rotating in planes at angles to each other and combined generically with means for eecting such cordinary indication registration or both.

Having thus fully defined the invention, what T claim as new and desire to secure by Letters Patent, is:

1. Tn a ygyroscopic compass for use on a moving vessel, vthe combination of a gyroscopic disk, means associated with said disk for indicating the true north; means associated with said disk for transmitting its indications to a` distant point; and gyroscopic means associated with said disk tendin to prevent compass errors de to the ro lingand pitching movements of the vessel, substantially as described.

2. lin a gyroscopic compass for use on a moving vessel the combination of a gyroscopic disk, means associated with said disk for indicating the true north; means associated with said disk for transmitting its yindications to a distant point; ysupporting means associated with said disk adapted to' generate friction as the ship moves in azimuth; automatic means for compensating for compass errors-due to the friction generated by said supporting means; and pendulous gyroscopic means associated with said disk tending to prevent compass errors due to the rolling and itching movements of the vessel, substantia ly as descrbed.`

Tn testimon whereof T amr my signature in presence o two witnesses.

MERVYN EDWARD CARRE-i".

Witnesseszr Cime. G. ANnnnsoia,

Granen A.. Rosenau..

titiV lill@ llllh 

